JPS58114305A - Magnetic recording and reproducing device - Google Patents

Magnetic recording and reproducing device

Info

Publication number
JPS58114305A
JPS58114305A JP21130181A JP21130181A JPS58114305A JP S58114305 A JPS58114305 A JP S58114305A JP 21130181 A JP21130181 A JP 21130181A JP 21130181 A JP21130181 A JP 21130181A JP S58114305 A JPS58114305 A JP S58114305A
Authority
JP
Japan
Prior art keywords
signal
flutter
wow
frequency
control
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
JP21130181A
Other languages
Japanese (ja)
Other versions
JPS6256593B2 (en
Inventor
Seisuke Hirakuri
平栗 晴介
Taku Uchiumi
内海 卓
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Victor Company of Japan Ltd
Nippon Victor KK
Original Assignee
Victor Company of Japan Ltd
Nippon Victor KK
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Victor Company of Japan Ltd, Nippon Victor KK filed Critical Victor Company of Japan Ltd
Priority to JP21130181A priority Critical patent/JPS58114305A/en
Publication of JPS58114305A publication Critical patent/JPS58114305A/en
Publication of JPS6256593B2 publication Critical patent/JPS6256593B2/ja
Granted legal-status Critical Current

Links

Classifications

    • GPHYSICS
    • G11INFORMATION STORAGE
    • G11BINFORMATION STORAGE BASED ON RELATIVE MOVEMENT BETWEEN RECORD CARRIER AND TRANSDUCER
    • G11B20/00Signal processing not specific to the method of recording or reproducing; Circuits therefor
    • G11B20/22Signal processing not specific to the method of recording or reproducing; Circuits therefor for reducing distortions
    • G11B20/225Signal processing not specific to the method of recording or reproducing; Circuits therefor for reducing distortions for reducing wow or flutter

Landscapes

  • Engineering & Computer Science (AREA)
  • Signal Processing (AREA)
  • Signal Processing Not Specific To The Method Of Recording And Reproducing (AREA)

Abstract

PURPOSE:To eliminate the wow and flutter of a reproduced sound signal, by eliminating the wow and flutter of a sound signal with a pilot signal which is separated from a signal modulated by a control signal. CONSTITUTION:A signal 30 modulated by a control signal is applied to a frequency divider 38 and a BBD39 via a zero-cross detector 36. The divided signals are supplied to clock driving circuits 42 and 43 via a PLL40 and a VCO41 respectively. Thus the clock pulses are generated in response to the wow and flutter to drive the BBDs39, 52 and 53. The output from which the wow and flutter of >=1Hz is eliminated by the BBD39 is fed to a clock driving circuit via a zero-cross detector 44, a PLL45 and a VCO58. The BBDs56 and 57 are driven by the output of the clock driving circuit. For sound signals 46 and 47, the wow and flutter of 1Hz is eliminated by LPFS350 and 51 and BBDs52 and 53 along with the wow and flutter of >=10Hz eliminated by the BBDs56 and 57 respectively and then delivered 67 and 68 via LPFs61 and 62.

Description

【発明の詳細な説明】 本発明は磁気記録再生装置に係シ、パイロット信号をコ
ントロール信号で変調し良信号をコントロールトラック
に記録し、再生された被変調波信号よプパイロット信号
を分離してこのパイロット信号の周波数変動を用いて音
声信号のワク・フラッタを除去することによシ、1本の
トラックでコントロール信号及びパイロット信号が記録
再生でき、再生された音声信号のワウ・フラッタを除去
できる磁気記録再生装置を提供することを目的とする。
DETAILED DESCRIPTION OF THE INVENTION The present invention relates to a magnetic recording and reproducing device, which modulates a pilot signal with a control signal, records a good signal on a control track, and separates the reproduced modulated wave signal and the pilot signal. By using this frequency fluctuation of the pilot signal to remove wow and flutter from the audio signal, the control signal and pilot signal can be recorded and played back on one track, and the wow and flutter from the reproduced audio signal can be removed. The purpose of the present invention is to provide a magnetic recording/reproducing device.

従来のビデオチーブレコーダにおいては、記録時に音声
信号と異なったトラックにFR波数略5OHHのコント
ロール信号を記録し、再生時に再生されたコントロール
信号と回転ドラムパルス又は基準信号発生器の基準信号
と位相比較してキャブスタンモータ回転制御を行ない、
かつ、キャプスタンフライホイールのPG発僚器よシの
信号から回転速度を検出してキャプスタンモータの回転
制御を行ない、再生音声信号にワウ・フラッタが含まれ
ないようしてい丸。しかし、このキャプスタンモータの
回転制御だけでは充分にジッタが取シ除かれず、再生音
声信号に含まれるワク・フラッタによ〕音質が悪化する
という欠点があった。
In a conventional video chip recorder, a control signal with an FR wave number of approximately 5OHH is recorded on a different track from the audio signal during recording, and during playback, the phase of the reproduced control signal is compared with a rotating drum pulse or a reference signal from a reference signal generator. to control the rotation of the cab stan motor.
In addition, the rotation speed of the capstan flywheel is detected from the signal from the PG transmitter, and the rotation of the capstan motor is controlled to prevent wow and flutter from being included in the reproduced audio signal. However, this rotational control of the capstan motor alone does not remove jitter sufficiently, and there is a drawback that the sound quality deteriorates due to jitter and flutter contained in the reproduced audio signal.

本発明は上記の欠点を除去したものであシ、以下図面と
共にその1実施例につき説明する。
The present invention eliminates the above-mentioned drawbacks, and an embodiment thereof will be described below with reference to the drawings.

jllH図は本発明装置の記録系の1実施例のブロック
系統図を示す、同図中、1Fi映倫信号の入来する入力
端子であり、この映倫信号は同期信号分離回路2に供給
される。同期信号分離回路2にょシ映偉信号から取シ出
された水平同期信号及び垂直同期信号は垂直同期信号分
離回路3に供給され、ここで第2図体〕に示す周波数略
@ OHzの垂直同期信号が分離されて分局器4に供給
される。分局器4はこの垂直同期信号を172分周して
第2図に)に示す周波数略30 Hzのパルスとしてこ
れを単安定マルチバイブレータ(以下「モノマルチ」ト
いう)5#6及び位相比較器Tに供給する。位相比較器
?Fi電圧制御発振器(以下「vOo」という)、分局
湯口と共にフェーズ・ロックド・ループ(以下「PLL
Jという)を構成しておp1分RSSによ)その発振周
波数を/  分周され九WOO16s暮4 0の出力信号が周波数略3 (l Htxのパルスと位
相比較されることによfi、Toolよシ周波数略畠・
Hzのパルスと同期のとれた周波数略4・1.・kHs
*のパルスが取〕出されてカウンター0の計数入力端子
に供給される。また、モノマルチSはM2図に)に示す
パルスの立上りによりトリガーされて第1図(0)に示
すパルスを発生しこれをカウンター0のリセット趨子に
供給し、モノマルチ・は第2図の)のパルスの立上シに
よりトリガーされて第1図(ロ)に示すパルス状のコン
トロール信号を発生しこれを変調器11に供給する。
Figure jllH shows a block system diagram of one embodiment of the recording system of the apparatus of the present invention. In the figure, it is an input terminal to which a 1Fi Eirin signal is input, and this Eirin signal is supplied to the synchronization signal separation circuit 2. The horizontal synchronizing signal and vertical synchronizing signal extracted from the digital signal are supplied to the vertical synchronizing signal separating circuit 3, where the vertical synchronizing signal with a frequency of approximately @OHz as shown in the second figure is extracted. is separated and supplied to the splitter 4. The divider 4 divides this vertical synchronizing signal by 172 and converts it into a pulse with a frequency of approximately 30 Hz as shown in Fig. 2. Supply to T. Phase comparator? Fi voltage controlled oscillator (hereinafter referred to as ``vOo''), phase-locked loop (hereinafter referred to as ``PLL'') together with a branch gate.
The oscillation frequency is divided by RSS, and the output signal of 9 WOO16S 40 is compared in phase with the pulse of Htx, which has a frequency of about 3 (l). Yoshi frequency summary Hatake
Frequency synchronized with Hz pulse approximately 4.1.・kHz
The * pulse is taken out and supplied to the counting input terminal of counter 0. In addition, the mono-multi S is triggered by the rising edge of the pulse shown in figure M2) and generates the pulse shown in figure 1 (0), which is supplied to the reset terminal of counter 0, and the mono-multi is shown in figure 2. Triggered by the rising edge of the pulse (), a pulse-like control signal shown in FIG. 1(b) is generated and supplied to the modulator 11.

カウンター0はモノマルチ5よりの第2図(0)に示す
パルスが立下った時点よj)VOOIから供給されるパ
ルスの計数を開始して、このパルスを/1・24分周し
て第2図(7)に示す周波数略4HHzのパルス(パイ
ロット信号)を発生してこれを低域フィルタ12に供給
する。ここでか忰、モノマルチ50時定数を調整して第
2図(0)に示すパルスのパルス幅を変えることにょル
第2図(7)に示すパルスの位相を進めたり遅らし九ル
することができる。第2図に)に示すパルスは低域フィ
ルタ12にょ夛高調波成分を除去されて両波数略410
 HIEの正弦波とされて変調器11に供給される。変
調器11#iこの周波数略410 Hstの正弦波をモ
ノマルチ6よシのパルスで振幅変調して、第2図(7)
に示す如くモノマルチ馨よ〕のパルスのローレベル期間
で振幅が大とな〕ハイレベル期間で振幅が小となる周波
数略4@OHaの変調波を発生しこれを増幅器1sに供
給する。この第2図(7)に示す被変調波は、モノマル
チ20時定数を変えることによシ大振幅から小振幅に変
化する点aの位相を変えることができ、モノマルチ1の
時定数を変えて第2図(至)のパルス幅を変えることに
より小振幅から大振幅に変化する点すの位相を変えるこ
とができ、変調器11において振幅Cを過轟なレベルと
することができる。
The counter 0 starts counting the pulses supplied from the VOOI at the time when the pulse shown in Figure 2 (0) from the monomulti 5 falls, and divides this pulse by /1.24 to count the pulses. A pulse (pilot signal) having a frequency of approximately 4 Hz as shown in FIG. 2 (7) is generated and supplied to the low-pass filter 12. At this point, you can adjust the monomulti 50 time constant to change the pulse width of the pulse shown in Figure 2 (0) or advance or retard the phase of the pulse shown in Figure 2 (7). be able to. The pulse shown in FIG.
The signal is supplied to the modulator 11 as a HIE sine wave. Modulator 11 #i Amplitude modulates this sine wave with a frequency of approximately 410 Hst using a monomulti 6 or higher pulse, as shown in Fig. 2 (7).
As shown in FIG. 1, a modulated wave having a frequency of approximately 4@OHa is generated and the amplitude is large during the low level period of the monomultiple pulse and small during the high level period, and this is supplied to the amplifier 1s. The phase of the modulated wave shown in Fig. 2 (7) can be changed by changing the time constant of the monomulti 20 at point a where it changes from large amplitude to small amplitude, and the time constant of monomulti 1 can be changed. By changing the pulse width shown in FIG. 2 (to), it is possible to change the phase of the pulse that changes from a small amplitude to a large amplitude, and the amplitude C in the modulator 11 can be made to an excessively loud level.

この被変調波は増幅器13において増幅された後混合器
14でバイアス発振器1sよシのバイアス信号に重畳さ
れて磁気ヘッド1@に供給され磁気テープITO長手方
向のコントロールトラックに記録される。これと共に入
力端子111 、1・bよ〕入来する第1チヤンネル、
第2チヤンネルの音声信号は夫々増幅器111L 、 
11に+で増幅された後混合器20& 、 201)に
おいて夫々バイアス発振器1iよりのバイアス信号に重
畳されて磁気ヘッド21a。
This modulated wave is amplified in an amplifier 13, then superimposed on a bias signal from a bias oscillator 1s in a mixer 14, and supplied to the magnetic head 1@, where it is recorded on a control track in the longitudinal direction of the magnetic tape ITO. Along with this, the first channel coming from the input terminal 111, 1/b,
The audio signals of the second channel are transmitted through amplifiers 111L and 111L, respectively.
11 and then superimposed on the bias signal from the bias oscillator 1i in mixers 20 & 201), respectively, to the magnetic head 21a.

Hl)に供給され磁気チーブ17の長手方向の上記コン
トロールトラックとは異なる2つの音声トラックに夫々
記録される。
HL) and are recorded on two audio tracks different from the control track in the longitudinal direction of the magnetic chip 17, respectively.

第3図は本発明になる磁気配録再生装置の再生系の1実
施例のブロック系統図を示す。5ori磁気テーグ1T
のコントロールトラックより再生されたjl!2図(I
F)K示す如き被変調波が入来する入力端子であplこ
の被変調波は自動利得制御(以下[ムGOJという)増
幅器31に供給されここで周期の長いレベル変動を除去
されつつ増幅されて復調器32及びリミッタ33に供給
される・復調器S!はこの被変調波を全波整流して第4
図■に示す波形としこれを平滑してIIJ図に)に示す
波形を得、これをゼロクロス検出器34に供給する。
FIG. 3 shows a block system diagram of one embodiment of the reproduction system of the magnetic recording and reproduction apparatus according to the present invention. 5ori magnetic tag 1T
jl! played from the control track of Figure 2 (I
F) An input terminal into which a modulated wave as shown in K is input. This modulated wave is supplied to an automatic gain control (hereinafter referred to as GOJ) amplifier 31, where it is amplified while removing long-period level fluctuations. Demodulator S! is supplied to the demodulator 32 and limiter 33. The modulated wave is full-wave rectified and the fourth
The waveform shown in FIG. 2 is smoothed to obtain the waveform shown in FIG.

ゼロクロス検出器34はこの第4図に)に示す波形を実
線dのスレッショールドレベルと比較して第4図(0)
に示すコントロール信号を検出してこれを出力端子3I
よシ出力する。ここで、コントロール信号の検出点・は
記録−におけるコントロール信号の発生した点である第
4図(4)の振幅の変化点aとの位相ずれfがあるが、
この位相ずれは復調器l叩の平滑時定数及びゼロクロス
検出器34のスレッショールドレベルにより決定され一
定な値であるため、従来と同様に精度の高いトラッキン
グが行なえる。
The zero cross detector 34 compares the waveform shown in FIG.
Detects the control signal shown in and outputs it to output terminal 3I.
Output. Here, there is a phase shift f between the detection point of the control signal and the amplitude change point a in FIG. 4 (4), which is the point where the control signal was generated during recording.
Since this phase shift is determined by the smoothing time constant of the demodulator I and the threshold level of the zero-cross detector 34 and is a constant value, highly accurate tracking can be performed as in the conventional case.

を九、ムGo増幅器31よシの被変調波はリミッタ13
でその振幅を一定とされた後ゼロクロス検出器S@に供
給され、ここでgv以上でハイレベル、Ov以下でロー
レベルとなるパルス状のコントロール信号とされてスイ
ッチaWの端子SW。
9, the modulated wave from the Go amplifier 31 is the limiter 13
After its amplitude is made constant, it is supplied to the zero cross detector S@, where it is converted into a pulse-like control signal that becomes high level above gv and low level below Ov, and is sent to terminal SW of switch aW.

及びPIIa 37に供給サレる。PLL57H供給さ
れるパルス状のパイロット信号の周波数変動に追従する
よう設定されておシ、パイロット信号がドロップアウト
した場合も内蔵したVaOの可変範囲内で発振を続はド
ロップアウトしたパルスを生成してスイッチ8Wの端子
8W2へ出力する。スーイツチ8Wはパイロット信号の
ドロップアウトがない場合端子sw、sw、を接続し、
ドロップアクトがある場合端子sw、swsを接続する
よう切換えるスイッチであシ、このスイッチSWを介し
て周波数略4・Q Haのパルスとされたパイロット信
号が分局器sl及びパケット・ブリゲート・デイノイイ
ス(以下「BBD Jという)3@に供給される。
and supplied to PIIa 37. PLL57H is set to follow the frequency fluctuation of the pulsed pilot signal supplied, and even if the pilot signal drops out, it continues to oscillate within the variable range of the built-in VaO and generates a dropped pulse. Output to terminal 8W2 of switch 8W. Switch 8W connects terminals sw and sw when there is no pilot signal dropout,
If there is a drop act, there is a switch that connects the terminals sw and sws. Through this switch SW, the pilot signal, which is made into a pulse with a frequency of about 4.Q Ha, is sent to the splitter sl and the packet brigade denoise (hereinafter referred to as It is supplied to 3@ (referred to as BBD J).

分周器■は上記パルスを176分周して周波数略1 @
 EmlのパルスとしてPI、I、40に供給する。こ
れは周波数略480 Hgのパイロット信号で低周波数
の周波数変動を検出するのは困離なため分周を行なって
周波数略1 @ Hzとしている。周波数略S・Hzの
パルスよりPLI、40において略1H馬以上の周波数
変動(ワウ・フラッタ)が検出されてPLL4oo内R
fるルーグフィルタよp電圧変化として*ciさtLV
QO41に供給さtL、70041はワク・フラッタに
応じすその発振周波数を変化させる。このvao41で
発生され大信号はクロックドライブ回路42.43に供
給され、ここでBBD用のクロックパルスに波形整形さ
れる。このクロックドライブ回路42.48は同じ特性
でクロックドライス回路1つで2つのBBDLが駆動で
きないため2つのクロックドライブ回路が使用される。
Frequency divider ■ divides the above pulse by 176 to give a frequency of approximately 1 @
It is supplied to PI, I, 40 as a pulse of Eml. Since it is difficult to detect low frequency fluctuations with a pilot signal having a frequency of approximately 480 Hg, the frequency is divided to a frequency of approximately 1@Hz. From a pulse with a frequency of approximately S.Hz, a frequency fluctuation of approximately 1H horse or more (wow/flutter) was detected at PLI, 40, and R in PLL4oo was detected.
As the p voltage change due to the Loog filter, *citLV
tL, 70041 supplied to QO41 changes the oscillation frequency of the base in accordance with the fluctuation and flutter. The large signal generated by this vao 41 is supplied to clock drive circuits 42 and 43, where it is waveform-shaped into a clock pulse for BBD. The clock drive circuits 42 and 48 have the same characteristics and cannot drive two BBDLs with one clock drive circuit, so two clock drive circuits are used.

1つで3つのBBDを駆動できればクロックドライブ回
路Fi1つで良い。クロックドライブ回路42にて得ら
れたクロックパルスはBBDslに供給され、BBDS
lはその遅延時間を可変することにより上記ワク・フラ
ッタを含んだ周波数略410 Hgのパイロット信号よ
り略IHM以上のワク・フラッタを除去した後ゼロクロ
ス検出器44に供給され、ここでまず低域フィルタ(図
示せず)によりクロック成分を除去された後ゼロクロス
検出されてパルスに整形されPLL4gに供給される。
If one clock drive circuit Fi can drive three BBDs, one clock drive circuit Fi is sufficient. The clock pulse obtained by the clock drive circuit 42 is supplied to BBDsl, and the BBDS
l is supplied to the zero-cross detector 44 after removing work and flutter of approximately IHM or higher from the pilot signal with a frequency of approximately 410 Hg including the work and flutter by varying its delay time, where it is first passed through a low-pass filter. After the clock component is removed by (not shown), the zero cross is detected, shaped into a pulse, and supplied to the PLL 4g.

を九、入力端子4’@ 、 4 Fに夫々入来する第1
チヤンネル、第2チヤンネルの音声信号は、夫々可変抵
抗4@、41で入力感度の調整をされ、低域フィルタs
o、stでBBDで転送ができない高域成分を除去され
夫々BBDS2.S1に供給サレル。C(DBBDS2
.53flBID$1と同じ段数のものであり上記□ク
ロックドライブ回路4sより供給されるクロックパルス
によりその遅延時間を可変させて夫々第1.第2チヤン
ネルの音声信号よ〕略I Hg以上のワウ・フラッタを
除去して低域フィルタ54.55に供給する。第1.第
2チヤンネルの音声信号は夫々低域フィルタs4゜5S
によfiBBD52.51で混入し九クロック成分を除
去されてBBDSl、STK供給される。
9, the first input to input terminals 4'@ and 4F, respectively.
The input sensitivity of the channel and second channel audio signals is adjusted by variable resistors 4@ and 41, respectively, and the input sensitivity is adjusted by the low-pass filter s.
o and st, high-frequency components that cannot be transferred by BBD are removed, and BBDS2. Sarel supplied to S1. C(DBBDS2
.. It has the same number of stages as the 53flBID$1, and its delay time is varied by the clock pulse supplied from the □clock drive circuit 4s, and the 1st. The second channel audio signal is supplied to low-pass filters 54 and 55 after removing wow and flutter of approximately I Hg or more. 1st. The audio signals of the second channel are each passed through a low-pass filter s4゜5S.
The nine clock components mixed in by fiBBD52.51 are removed and supplied to BBDS1 and STK.

ここで、略I Hg以上のワク・フラッタを除去する九
めには、BBDSl 、52 、!13(D遅g時間の
可変範囲を大きくする必要があり、BIIDS@。
Here, the ninth step to remove the work and flutter of about I Hg or more is BBDSl,52,! 13 (It is necessary to widen the variable range of D delay g time, BIIDS@.

52、$3の遅延時間は長く設定されている。このため
、周波数の高い(たとえば1g五厘以上)のワウ・フラ
ッタについては遅延による位相遅れが大となってこれを
除去できず、BBDSl、II。
52, the delay time of $3 is set to be long. Therefore, for wow and flutter with a high frequency (for example, 1 g or more), the phase lag due to the delay becomes large and cannot be removed.

ssの出力であるパイロット信号、第1.第2チヤンネ
ルの音声信号にはこの周波数の高いフラッタ成分が同様
に含まれている。
The pilot signal which is the output of ss, the first. The second channel audio signal similarly contains this high frequency flutter component.

BBI)IIにより周波数の低いワク・フラッタを除去
されゼロクロス検出器44で波形整形された周波数路4
HI Hzのパイロット信号FiPLL41に供給され
る。この周波数路4・Q HzのパルスはPLL41に
おいて略1・H8以上の周波数変動(フラッタ)が検出
されてpLL 45の内蔵するループフィルタよ〕電圧
変化として取〕出されvoOI−に供給される。VOO
lgはフラッタに応じてその発振周波数を変化させ、こ
れをクロックドライブ回路@Oに供給し、ここで波形整
形されて得られたクロックパルスがBBD!!@、IF
K供給される。BBD51.SFは段数が等しく19〜
S OHzのフラッタを除去するに最適な遅延時間とさ
れている。BBDS@、ITは夫々クロックドライブ回
路層Oよりのクロックパルスにより遅延時間を可変させ
て、第1.第2チヤンネルの音声信号よ61トI@H2
+のフラッタを除去して低域フィルタ@1.@2に供給
する。第1.第2チヤンネルの音声信号は夫々低域フィ
ルタ@1.@1でBBDS@、5Fで混入したクロック
成分を除去された後、増幅器6g、@4で増幅され可変
抵抗@S、@・で出力レベルを調整されて出力端子sy
、@sよ〕出力される。
Frequency path 4 whose low frequency fluctuations and flutter are removed by BBI) II and whose waveform is shaped by the zero cross detector 44
A HI Hz pilot signal is supplied to the FiPLL 41. A frequency fluctuation (flutter) of approximately 1.H8 or more is detected in the PLL 41 of this frequency path 4.Q Hz pulse, which is extracted as a voltage change by the loop filter built in the pLL 45 and supplied to voOI-. VOO
lg changes its oscillation frequency according to the flutter and supplies it to the clock drive circuit @O, where the waveform is shaped and the resulting clock pulse is BBD! ! @, IF
K is supplied. BBD51. SF has the same number of stages, 19~
This is considered to be the optimum delay time for removing SOHz flutter. BBDS@ and IT each vary the delay time using a clock pulse from the clock drive circuit layer O, and the first. 2nd channel audio signal 61t I@H2
+ flutter is removed and low-pass filter @1. Supply @2. 1st. The audio signals of the second channel are respectively low-pass filtered @1. After the clock component mixed in with BBDS@ and 5F is removed with @1, it is amplified with amplifier 6g and @4, and the output level is adjusted with variable resistors @S and @・, and output terminal sy
, @s] is output.

ここで、記録時における第2図(F)に示す被変調波の
大振幅から小振幅に変化する点10位相と、再生された
音声信号に含まれるワク・フラッタとの間には第5図に
示す如き関係がある。第S図は第2図(7)に示す大振
幅の正弦波が最小値をとる点が上記変化点aであるとき
その位相なOとしてこの位相を士t (ra4:l変化
させ、再生された音声信号に含まれるワク・フラッタを
測定したものである。#!5図より明らかなように変化
点1の位相が略Oであるとき最もワウ・フラッタが少な
く、この変化点10位相を第1図に示すモノマルチSの
時定数を変化させることにより略Oにすることができる
Here, there is a difference between the point 10 phase at which the modulated wave changes from large amplitude to small amplitude shown in Fig. 2 (F) during recording and the fluctuations and flutters included in the reproduced audio signal as shown in Fig. There is a relationship as shown below. Figure S shows that when the point where the large-amplitude sine wave shown in Figure 2 (7) takes its minimum value is the above-mentioned change point a, this phase is changed to This is a measurement of the wow and flutter contained in the audio signal. As is clear from Figure #!5, when the phase of change point 1 is approximately O, the wow and flutter is the least, and this change point 10 phase is the By changing the time constant of the monomulti S shown in FIG. 1, it can be made approximately O.

上述の如く、本発明になる磁気記録再生装置は、音声信
号を磁気記録媒体の長手方向の音声トラックに記録する
と共に映僚信号の喬直同期信号から得られるコントロー
ル信号より生成されコントロール信号周波数の整数倍の
周波数であるパイロット信号をコントロール信号によ〕
変調して被変調波を得、被変調波を音声トラックとは異
なる磁気記録媒体長手方向のコントロールトラックに記
録し、コントロールトラックよシ再生された被変調波を
復調してコントロール信号を得ると共に被変調波からコ
ントロール信号と同期−のとれたバイロッジ信号を分離
し、このパイロット信号の周波数変動を検出して音声ト
ラックよシ再生された音声信号に含まれるワク・フラッ
タを除去するため、従来コントロール信号のみが記録再
生されていたコントロールトラックを用いてコントロー
ル信号及びパイロット信号の記録再生ができ、このパイ
ロット信号の周波数変動から従来除去できなかつ九ワウ
・フラッタを除去して歪のない音声信号を得ることがで
きる等の轡長な有するものである。
As described above, the magnetic recording/reproducing apparatus according to the present invention records an audio signal on an audio track in the longitudinal direction of a magnetic recording medium, and also records a control signal frequency generated from a control signal obtained from a direct synchronization signal of a video signal. A pilot signal with a frequency that is an integer multiple is used as a control signal]
The modulated wave is modulated to obtain a modulated wave, the modulated wave is recorded on a control track in the longitudinal direction of the magnetic recording medium that is different from the audio track, and the modulated wave reproduced from the control track is demodulated to obtain a control signal and the modulated wave is In order to separate the bilodge signal synchronized with the control signal from the modulated wave and detect the frequency fluctuation of this pilot signal to remove fluctuations and flutter contained in the audio signal reproduced from the audio track, conventional control signals are used. To record and reproduce a control signal and a pilot signal using a control track on which only a control signal was recorded and reproduced, and to obtain a distortion-free audio signal by removing wow and flutter, which cannot be removed conventionally, from the frequency fluctuation of this pilot signal. It is something that has the length to be able to do things.

【図面の簡単な説明】[Brief explanation of the drawing]

第1図は本発明装置の記録系の1実施例のブロック系統
図、第2図に)〜V)は第1図示の回路各部の信号波形
を示すタイムチャート、第3図は本発明装置の再生系の
ml!施例のブロック系統図、第4図(4)〜(C) 
U第3図示の回路各部の信号波形を示すタイムチャート
、第S図は変調信号が大振幅から小振幅に変化する点の
位相と再生音声信号に残つ九ワウ・フラッタの関係を示
す図である。 ? 、 IIIL 、 1−1) 、 30 、41 
、47−・・入力端子、2・・・同期信号分離回路、3
・・・垂直同期信号分離回路、4,1.II・・・分周
器、5,6・・・モノマルチ、7−・・位相比較器、I
 、41 、If・VOo、1 @・・・カウンタ、1
1・・・変調器、?!、$0.If。 54.55.@1.@2・・・低域フィルタ、13゜B
BI亀、 181) 、・3.@4・・・増幅器、14
,211&。 20m)・・・混合器、1s・・・バイアス発振器、1
6゜21a 、 ztb・・・磁気ヘッド、IT・・・
磁気テープ、31・・・ムGO増幅器、32・・・複調
器、33・・・91ツタ、$4.ll、44・・・ヤロ
クロス検出器、37.40.45−PLL、$1.52
.Is。 1@ 、IT・ BBD、42.48 、@@−・・ク
ロックドライブ回路、@1.@ト・・出力端子。
FIG. 1 is a block system diagram of one embodiment of the recording system of the apparatus of the present invention, FIG. 2) to V) are time charts showing signal waveforms of each part of the circuit shown in FIG. Reproduction ml! Block system diagram of the example, Fig. 4 (4) to (C)
Figure U is a time chart showing the signal waveforms of each part of the circuit shown in Figure 3. Figure S is a diagram showing the relationship between the phase of the point where the modulation signal changes from large amplitude to small amplitude and the nine wow and flutter that remains in the reproduced audio signal. be. ? , IIIL, 1-1), 30, 41
, 47--Input terminal, 2--Synchronization signal separation circuit, 3
...Vertical synchronization signal separation circuit, 4,1. II... Frequency divider, 5, 6... Mono multi, 7-... Phase comparator, I
, 41 , If・VOo, 1 @... counter, 1
1...Modulator? ! , $0. If. 54.55. @1. @2...Low pass filter, 13°B
BI Kame, 181),・3. @4...Amplifier, 14
, 211&. 20m)...Mixer, 1s...Bias oscillator, 1
6゜21a, ztb...magnetic head, IT...
Magnetic tape, 31...Mugo amplifier, 32...Bitonizer, 33...91 Ivy, $4. ll, 44... Yarocross detector, 37.40.45-PLL, $1.52
.. Is. 1@, IT/BBD, 42.48, @@-...Clock drive circuit, @1. @T... Output terminal.

Claims (2)

【特許請求の範囲】[Claims] (1)  音声信号を磁気記録鳥体の長手方向の音声ト
ラックに記録すると共に映偉信号の一厘同期信号から得
られるコントロール信号よ〕生成され骸コントロール信
号周波数の整数倍の周波数であるパイロット信号を咳コ
ントロール信号により変調して被変調波を得、該被変調
波を該音声トラックとは異なる該磁気記録媒体長手方向
のコントロールトラックに記録し、誼コントロールトラ
ックよ〕再生され圧波変調波を復調してコントロール信
号を得ると共に該変調波から該コントロール信号と同期
のとれ九パイロット信号を分離し、誼パイロット信号の
周波数変動を検出して該音声トラックより再生された音
声信号に含壕れるワク・フラッタを除去することを特徴
とする磁気記録再生装置・
(1) The audio signal is recorded on the audio track in the longitudinal direction of the magnetically recorded bird body, and the control signal obtained from the synchronous signal of the video signal is generated] A pilot signal whose frequency is an integral multiple of the frequency of the control signal is generated. is modulated by a cough control signal to obtain a modulated wave, the modulated wave is recorded on a control track in the longitudinal direction of the magnetic recording medium that is different from the audio track, and the pressure wave modulated wave is demodulated by being reproduced from the control track. At the same time, a control signal is obtained, and a pilot signal that is synchronized with the control signal is separated from the modulated wave, and the frequency fluctuation of the pilot signal is detected to detect the noise contained in the audio signal reproduced from the audio track. Magnetic recording and reproducing device characterized by eliminating flutter.
(2)峡被変調波F!、誼パイロット信号を該コントロ
ールによシ振幅変調して得られることを特徴とする特許
請求の範囲第fXJXt!載の磁気記録再生装置。
(2) Gorges modulated wave F! , is obtained by amplitude modulating the pilot signal using the control, Claim fXJXt! Magnetic recording and reproducing device.
JP21130181A 1981-12-25 1981-12-25 Magnetic recording and reproducing device Granted JPS58114305A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP21130181A JPS58114305A (en) 1981-12-25 1981-12-25 Magnetic recording and reproducing device

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP21130181A JPS58114305A (en) 1981-12-25 1981-12-25 Magnetic recording and reproducing device

Publications (2)

Publication Number Publication Date
JPS58114305A true JPS58114305A (en) 1983-07-07
JPS6256593B2 JPS6256593B2 (en) 1987-11-26

Family

ID=16603671

Family Applications (1)

Application Number Title Priority Date Filing Date
JP21130181A Granted JPS58114305A (en) 1981-12-25 1981-12-25 Magnetic recording and reproducing device

Country Status (1)

Country Link
JP (1) JPS58114305A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0354059A2 (en) * 1988-08-04 1990-02-07 Archive Corporation Method and apparatus for removing data stream timing variations

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0354059A2 (en) * 1988-08-04 1990-02-07 Archive Corporation Method and apparatus for removing data stream timing variations

Also Published As

Publication number Publication date
JPS6256593B2 (en) 1987-11-26

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